航空兵器Issue(2)：9-15,7.
空基动能拦截弹制导控制系统建模与仿真
Modeling and Simulation of Guidance and Control System of Air-Borne Kinetic Energy Interceptor
摘要
Abstract
To study the guidance and control system of air-borne kinetic energy interceptor （KEI）, the engagement process for boost phase ballistic missile interception is explored, and the trajectory model of a ballistic missile during the boost phase is established. According to the boost phase flight characteristics of ballistic missile, the guidance and control system models of KEI are constructed, including the structural model, the dynamic and kinetic model, the relative movement model, the measurement model, the compound guidance model and the direct force/aerodynamic force control model. Under the environment of Matlab/Simulink, the digital simulation system is developed. The simulation results prove the fea- sibility and practicability of the model.关键词
弹道导弹/助推段拦截/空基动能拦截弹/制导控制Key words
ballistic missile/boost phase intercept/air-borne kinetic energy interceptor/guidanceand control分类
军事科技引用本文复制引用
肖增博,雷虎民,张蓬蓬,冯璐..空基动能拦截弹制导控制系统建模与仿真[J].航空兵器,2012,(2):9-15,7.基金项目
航空科学基金 （）
